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TECHNICAL PAPERS: Gas Turbines: Structures and Dynamics

Perturbations Methods in Structural Dynamics and Applications to Cyclic Symmetric Domains

[+] Author and Article Information
Bernard Lalanne

 TURBOMECA, 64511 Bordes, Francebernard.lalanne@turbomeca.fr

J. Eng. Gas Turbines Power 127(3), 654-662 (Dec 13, 2004) (9 pages) doi:10.1115/1.1924430 History: Received August 08, 2002; Revised December 13, 2004

The design of components must take into account the irregularities inherent to the manufacturing process. When the structures have close eigenvalues, small mass and stiffness variations or the damping generate strong variations of the eigenmodes: these structures are then not robust. Here, their dynamics has been analyzed by perturbation method, in the dissipative cases and with coupling within a light fluid. A new perturbation method allows first order developments whatever the spectral density may be. Applications to many different vibration problems are presented: aeroelasticity, mode veering problem, maximum amplitude of forced response in cyclic symmetric domains, with detuning and/or mistuning, i.e., the most important reliability problem in turbomachinery. The results of this study provide a new estimation of the amplification factor and damping due to mistuning and aerodynamic coupling.

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Copyright © 2005 by American Society of Mechanical Engineers
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Figures

Grahic Jump Location
Figure 1

Amplification factor with two modal perturbations

Grahic Jump Location
Figure 2

Bladed disk veering

Grahic Jump Location
Figure 3

Veering acoustic resonance-bladed disk mode

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